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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Twist-flex life, tensile properties, thermal expansion coefficient, and permeabilty of polymeric material for cryogenic propellant tank liners
Acoustic absorption liners for suppressing HF COMBUSTION instability in rocket engine combustion chambers
Glass flake and epoxy resin matrix for liner of filament-wound fiberglass cryogenic propellant tank structures
Ultrahigh vacuum chamber with liquid-helium-cooled liner for space environment simulation
Acoustic absorption liners for suppressing HF COMBUSTION instability in rocket engine combustion chambers
Large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner for space simulation
Liner extends the service life of high-angulation /26-degree/ bellows used as ducts for high-velocity fluid flow in a liquid oxygen fill and drain system. It consists of a conical frustum or nozzle on the upstream side and a cylindrical section or catcher on the down-stream side.
Experimental investigation of acoustic liners to suppress screech in hydrogen-oxygen engines
Tensile and interlaminar shear strengths of glass, boron, and graphite filament wound resin composites and liners for cryogenic pressure vessels
Boron and graphite filament-resin composites tensile and interlaminar shear strengths and Al foil liner cyclic life in cryogenic pressure vessel tests
Tensile strength properties of glass, boron, and graphite filament wound resin composites and liners for cryogenic pressure vessels
Small amplitude linear analysis of combustion instability with finite Mach number flow and acoustic liners
Experimental, and theoretical evaluations of acoustic liners for screech suppression in rocket engines
Hydrogen-oxygen rocket engine used to test acoustic liner with isolated resonators and variable cavity depths
Combustion instability with finite Mach number flow and acoustic liners
Axial and circumferential segmented combustor liners for turbojet engine
Behavior of convergent-divergent nozzles and acoustic liners in three dimensional acoustic fields
Glass, boron and graphite filament wound resin composites and liners for cryogenic pressure vessels